CIRRUS DESIGN CORP SR22

Full Narrative

On July 7, 2015, about 1137 central daylight time, a Cirrus SR-22 single-engine airplane, N422PB, descended under the canopy of the cirrus airframe parachute system (CAPS) and landed in a residential neighborhood at Houston, Texas. The pilot and passenger sustained minor injuries, and the airplane was substantially damaged. The airplane was registered to and operated by AIRCCS, LLC; Humble, Texas, as a Title 14 Code of Federal Regulations Part 91 business flight. Day visual meteorological conditions (VMC) prevailed, and a flight plan had not been filed. The airplane departed George Bush Intercontinental/Houston Airport (IAH), Houston, Texas, at 1133, and was destined for Austin Bergstrom International Airport (AUS), Austin, Texas.

The pilot reported that during initial climb, he noticed increasing engine temperatures, so he reduced power in an attempt to lower the engine temperatures. When the airplane was about 900 feet above ground level (agl), the engine started to "detonate," and soon after, there was a complete loss of engine power. With no suitable forced landing area, the CAPS was deployed, and the airplane impacted terrain and came to rest upright next to a residence.

An on-scene wreckage examination showed there was adequate fuel on-board, consistent with aviation low-lead fuel. At the facility where the airplane had most recently been refueled, refueling unit records and a review of security camera video showed that the airplane had been refueled with aviation gasoline and not with jet fuel.

Avionics components containing non-volatile memory (NVM), which included engine performance data, were sent to the National Transportation Safety Board (NTSB) Vehicle Recorder Division for download. A review of the data for the accident flight found the engine rpm reached at least 3,500 rpm (engine speed above 3,500 rpm would not be recorded, since the maximum valve for the sensor is 3,500 rpm). Per the engine's Type Certificate, the maximum engine speed is 2,700rpm.

A review of maintenance records for the airplane revealed the propeller governor had been removed and inspected for proper operation, prior to the accident flight. The records also noted that no defects were observed on the governor, and the governor was reinstalled by maintenance personnel.

During the post-accident examination, the governor was removed from the engine and tested at McCauley Propeller, Columbus, Georgia. The test revealed the governor operated within the specified parameters for the unit. The examination noted that the propeller governor attaching nuts were rounded off and the washers for the governor were improperly stacked.

The engine was also removed from the airframe and shipped to Continental Motors, Mobile, Alabama, for examination/disassembly. The examination found that the governor drive gear was fractured in half and located in the oil sump. The governor drive gear teeth exhibited damage consistent with the governor driven gear being misaligned. The governor drive gear teeth also exhibited damage. A broken governor drive gear would result in insufficient oil pressure to drive the propeller governor and cause an engine to over speed.

The pilot did not submit an NTSB Pilot/Operator Accident Report form (NTSB Form 6120.1).